EP0168145A2 - Non-linear control type magnetic bearing - Google Patents
Non-linear control type magnetic bearing Download PDFInfo
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- EP0168145A2 EP0168145A2 EP85303636A EP85303636A EP0168145A2 EP 0168145 A2 EP0168145 A2 EP 0168145A2 EP 85303636 A EP85303636 A EP 85303636A EP 85303636 A EP85303636 A EP 85303636A EP 0168145 A2 EP0168145 A2 EP 0168145A2
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- electromagnets
- magnetic bearing
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- 238000006073 displacement reaction Methods 0.000 claims abstract description 42
- 230000001133 acceleration Effects 0.000 claims abstract description 16
- 230000005284 excitation Effects 0.000 claims abstract description 14
- 238000010586 diagram Methods 0.000 description 4
- 238000001514 detection method Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000012886 linear function Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 238000004364 calculation method Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- 238000004146 energy storage Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000005339 levitation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000004088 simulation Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0406—Magnetic bearings
- F16C32/044—Active magnetic bearings
- F16C32/0444—Details of devices to control the actuation of the electromagnets
- F16C32/0451—Details of controllers, i.e. the units determining the power to be supplied, e.g. comparing elements, feedback arrangements with P.I.D. control
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0406—Magnetic bearings
- F16C32/044—Active magnetic bearings
- F16C32/0444—Details of devices to control the actuation of the electromagnets
- F16C32/0446—Determination of the actual position of the moving member, e.g. details of sensors
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C32/00—Bearings not otherwise provided for
- F16C32/04—Bearings not otherwise provided for using magnetic or electric supporting means
- F16C32/0406—Magnetic bearings
- F16C32/044—Active magnetic bearings
- F16C32/0474—Active magnetic bearings for rotary movement
- F16C32/0476—Active magnetic bearings for rotary movement with active support of one degree of freedom, e.g. axial magnetic bearings
Definitions
- This invention relates to a magnetic bearing used, for example, in a magnetically levitating apparatus and, in particular, a non-linear control type magnetic bearing.
- An object of this invention is to provide a non-linear control type magnetic bearing which obviates the necessity of providing any expensive position displacement sensor and power amplifier.
- Another object of this invention is to provide a non-linear control type magnetic bearing which can start to levitate an object from an at-rest position.
- Another object of this invention is to provide a non-linear control type magnetic bearing requiring a less power dissipation.
- the essence of this invention resides in that, in the non-linear control type magnetic bearing, the displacement of an object to be levitated is found based on the output signal of a velocity sensor and excitation current of electromagnets without the necessity of providing any expensive position displacement sensor and the need of using any expensive power amplifier is eliminated by a pair of electromagnets excited alternately.
- a non-linear control type magnetic bearing comprises (al) a pair of mutually opposite electromagnets, sandwiching an object to be levitated therebetween with a gap left between the electromagnet and the object, for attracting the object under their magnetic force; (a2) current supply means for alternately supplying excitation current to the respective electromagnets; (a3) a means for detecting the level of current flowing through the respective electromagnet and for generating a pair of current level signals; (a4) a velocity sensor for detecting a velocity with which the object to be levitated is moved in a direction in which the pair of electromagnets face each other and for generating a velocity signal; (a5) difference means for finding a difference between the pair of current level signals and for generating a difference signal; (a6) differentiating means for differentiating the velocity signal and for determining an acceleration rate of the object to generate an acceleration signal; (a7) analog operation means for performing an analog operation on an equation of motion of the object with the use of the difference signal and acceleration signal to find
- the above-mentioned non-linear control type magnetic bearing essentially possesses a levitation start function and thus implements an energy-saving effect analogous to a zero-power system. Furthermore, the magnetic bearing also performs a lift-off function in the gravitational field. Even if as a switching element use is made of a transistor, a switching amplifier can be compactized as it utilizes the switching amplifying principle in which the transistor is operated constantly at a minimum heat-generating region. This arrangement obviates the need of providing any expensive position displacement sensor and power amplifier. Therefore, an inexpensive magnetic bearing can be readily implemented having a contactless, non-friction and oilless feature.
- First and second electromagnets 12 and 14 are arranged opposite to each other in a manner to sandwich an object 10 therebetween with a gap left there. Coils of the first and second electromagnets 12 and 14 are connected at one end to one terminal of a power supply 16.
- the coil of the first electromagnet 12 is connected at the other end to an Sl terminal of a changeover switch 20 through a first resistor 18 for current detection and the coil of the second electromagnet 14 is connected at the other end to an S2 terminal of the changeover switch 20 through a second resistor 22 for current detection.
- An SO terminal of the changeover switch 20 is connected to the other terminal of the power supply 16.
- the first electromagnet 12 is excited with the Sl terminal of the changeover switch 20 in the ON state and the second electromagnet 14 is excited with the S2 terminal of the changeover switch 20 in the ON state. That is, the first and second electromagnets 12 and 14 are excited alternately.
- the changeover switch 20 is comprised of, for example, a transistor as a switching element.
- a velocity sensor 26 comprised of, for example, a search coil is disposed opposite to the lower surface of the object 10. The velocity with which the object 10 is moved up and down is detected by the velocity sensor 26 and a velocity signal dx/dt is supplied to the operating circuit 24.
- the operating circuit 24 is comprised of a subtracter 28, differentiator 30, analog operating circuit 32 and switching discriminator 34, as shown in Fig. 2.
- a difference signal i as an output of the subtracter 28 is supplied to the analog operating circuit 32.
- a velocity signal dx/dt which is detected at the velocity sensor 26 is supplied to the differentiator 30 where it is differentiated.
- the differentiated signal is supplied as the acceleration signal d 2 x/dt 2 , together with the current level signal, to the analog operating circuit 32.
- the current level signal i and acceleration signal d 2 x/dt 2 are substituted into the equation of motion of the object 10 to effect an analog operation and thus to produce a position displacement signal x of the object 10.
- the position displacement signal x is supplied, together with the velocity signal dx/dt, to the switching discriminator 34.
- the switching discriminator 34 identifies the positive or negative sign of a linear equation for the position displacement signal and velocity signal, and supplies to the changeover switch 20 a switching signal which alternately switches a supply of current to the electromagnets. It is to be noted that an origin 0 in the position displacement of the object is determined to be located at an equilibrium point of the object 10 as shown in Fig. 1.
- a force acting on the object 10 is comprised of a gravitational force and electromagnetic force. Now suppose only the electromagnetic force with the gravitational force disregarded here. Then, the equation of motion of the object 10 is given below:
- the optimal control is realized if switching is effected to f at F(x, dx/dt) > 0 or -f at F(x, dx/dt) ⁇ 0.
- f represents a constant.
- Equation (1) the right-handed side of Equation (1) is not a constant, but a function for the current level and position, presenting a problem.
- FIG. 3A and 3B and Figs. 4A and 4B show the loci of the simulations in the phase plane.
- the changeover switch 20 When the coil has a small time constant (L/R) and then a time delay of the current is small, the changeover switch 20 is switched to the Sl side at an initial level point A to permit the energization of the electromagnet 12 as shown in Fig. 3A. At the level point C, the changeover switch 20 is switched to the S2 side to permit the energization of the electromagnet 14. Thereafter, the displacement x of the object immediately reaches a target position 0 and thus an optimal control is realized with minimum time. This will be also well understood from the current level variation of the electromagnets 12 and 14 as shown in Fig. 3B. After the displacement x of the object has arrived at the 0 point, this state (the 0 state) is maintained by the frequent switching operations.
- L/R time constant
- T L/R
- R R > 0
- the embodiment of this invention adopts a switching line 0 with a limited gradient with respect to an origin 0 as shown in Fig. 5A.
- the switching curve P is shown for guidance only and can be derived from Equation (6). This is of the same type as shown in Figs. 3A and 4A.
- the switching curve P has an infinite gradient at the origin 0 and is different from the switching curve Q in this embodiment.
- the switching curve Q becomes a linear function for the displacement x and velocity signal dx/dt and thus is represented as follows:
- Fig. 5C shows a relation of the displacement x of the object to the time t. From Fig. 5C it is also found that the displacement of the object 10 converges toward the equilibrium point 0.
- Fig. 5D shows a variation of excitation currents iA, iB to the time t. From a comparison between Fig. 5D and Figs. 3B and 4B, it will be appreciated that the system of this embodiment needs a very small level of excitation current. Therefore, the embodiment of this invention, though being somewhat lower in response characteristics, can achieve a stability and a small power dissipation of practical importance.
- the switching discriminant H(x, dx/dt) is the linear function of the displacement x and velocity signal dx/dt, it is possible to very readily effect an analog computation.
- the value y in Fig. 5C is an estimated value of the control system which is obtained by finding the position of the object through the use of the equation of motion (1) under the assumption that there is no disturbance.
- the actual displacement x of the object 10 is in agreement with the estimated value y, provided that there is no disturbance.
- the object 10 is automatically moved to a position B where, as shown in Fig. 6A, the electromagnetic force of the electromagnets 12 and 14 and gravity are in static equilibrium, with the result that the object 10 is maintained at the position B.
- Fig. 6B shows a relation of the velocity dx/dt to the acceleration d 2 x/dt 2 .
- the estimated value y of the control system varies with the time t and the object 10 reaches an equilibrium point as shown in Fig. 6D.
- the excitation current of the coils varies as shown in Fig. 6E. It is to be noted that the ON time of the electromagnet 12 is somewhat longer than that of the electromagnet 14.
- the object 10 can be magnetically levitated by controlling the changeover switch 20 using a switching discrimination signal generated in the operating circuit 24.
- the currents through the electromagnets 12 and 14 are reduced to a very small level due to the impedance of the coils, thus involving a very small dissipation power. Therefore, the non-linear control type magnetic bearing of low cost can be implemented without the need of providing any expensive position displacement sensor and power amplifier.
- a judging circuit 40 is connected between a terminal SO of a changeover switch 20 and the end of a power supply 16 and adapted to judge whether or not the current from the power supply 16 continues for over a predetermined period of time at maximum.
- the judgment data is supplied to a switching discriminator 34 in an operating circuit 24.
- the object 10 can surely be levitated from an at-rest position under the action of the judging circuit 40 and operating circuit 24.
- the other arrangement of this embodiment is the same as that of the first embodiment of this invention. Therefore, further explanation is omitted.
- the object 10 is located, for example, on the side of the electromagnet 14 and the changeover switch 20 is placed on the side of the S2 terminal. Then, since the output of the velocity sensor 26 is 0, no immediate switching occurs at the changeover switch 20. During this time period, a maximum current continuously flows through the electromagnet 14 and the judging circuit 40 judges this state. The judgment data is supplied to the switching discriminator 34, causing the changeover switch 20 to be forcedly switched to the Sl terminal of the switch 20. Thereafter, the object 10 is automatically moved to a position 0 in the same way as explained in connection with Figs. 6A through 6E, and starts to be levitated.
- This invention is not restricted to the above-mentioned embodiments.
- a power relay may be used as the changeover switch in place of the transistor.
- the judging circuit 40 is not required to be connected between the power supply 16 and the changeover switch 20, and may be placed anywhere in the associated circuit so long as it can judge that maximum current flows through either of the electromagnets 12, 14 for over a predetermined period of time.
- Various changes or modifications can be made within the spirit and scope of this invention.
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- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
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- Mechanical Engineering (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
Description
- This invention relates to a magnetic bearing used, for example, in a magnetically levitating apparatus and, in particular, a non-linear control type magnetic bearing.
- A variety of magnetic bearings utilizing the attractive force of electromagnets have recently been developed, but this type of magnetic bearing is, in general, very expensive, since a position displacement sensor and power amplifier necessary for magnetic bearings are much higher in cost and greater in dissipation power. If these drawbacks are overcome, then it may be considered that such magnetic bearings having a contactless, non-friction and oilless feature will find a wider range of practical application.
- In the field of a linear control method, a magnetic bearing has already been implemented and commercialized which utilizes a velocity sensor using an inexpensive, easy-to-manufacture search coil in place of the expensive position displacement sensor. It is disclosed in, for example, "Magnetic Suspension with Passive Radial Centering for Satellite Flywheel and Kinetic Energy Storage Systems", the Third International Workshop on Rare Earth-Cobalt Permanent Magnets and Their Applications, June 27 to 30, 1978 by P.C. Poubeau. This system also has advantages as a "zero-power" system and has already been established as such. However, this system has a drawback that it cannot start to levitate an object from an at-rest position. For this reason, an extra lift-off circuit is provided so as to levitate the object. It is therefore necessary to provide another sensor corresponding to the position displacement sensor. This is a substantial bar to a wide acceptance of this system.
- A general non-linear type control theory is disclosed in A.A. πaBπOB "CHHTE3 PEπEb1X OΠTMAΠbHb1X ΠO 5b1CTPOΠECTBO", 1966. However, this theory has not been applied to magnetic bearings so far.
- An object of this invention is to provide a non-linear control type magnetic bearing which obviates the necessity of providing any expensive position displacement sensor and power amplifier.
- Another object of this invention is to provide a non-linear control type magnetic bearing which can start to levitate an object from an at-rest position.
- Another object of this invention is to provide a non-linear control type magnetic bearing requiring a less power dissipation.
- The essence of this invention resides in that, in the non-linear control type magnetic bearing, the displacement of an object to be levitated is found based on the output signal of a velocity sensor and excitation current of electromagnets without the necessity of providing any expensive position displacement sensor and the need of using any expensive power amplifier is eliminated by a pair of electromagnets excited alternately.
- A non-linear control type magnetic bearing according to this invention comprises (al) a pair of mutually opposite electromagnets, sandwiching an object to be levitated therebetween with a gap left between the electromagnet and the object, for attracting the object under their magnetic force; (a2) current supply means for alternately supplying excitation current to the respective electromagnets; (a3) a means for detecting the level of current flowing through the respective electromagnet and for generating a pair of current level signals; (a4) a velocity sensor for detecting a velocity with which the object to be levitated is moved in a direction in which the pair of electromagnets face each other and for generating a velocity signal; (a5) difference means for finding a difference between the pair of current level signals and for generating a difference signal; (a6) differentiating means for differentiating the velocity signal and for determining an acceleration rate of the object to generate an acceleration signal; (a7) analog operation means for performing an analog operation on an equation of motion of the object with the use of the difference signal and acceleration signal to find a position displacement of the object and for generating a position displacement signal; and (a8) switching discriminator means for identifying a positive or a negative sign of a linear equation of the position displacement signal and velocity signal and for supplying to the current supply means a switching signal for alternately switching a supply of current to the pair of electromagnets.
- The above-mentioned non-linear control type magnetic bearing essentially possesses a levitation start function and thus implements an energy-saving effect analogous to a zero-power system. Furthermore, the magnetic bearing also performs a lift-off function in the gravitational field. Even if as a switching element use is made of a transistor, a switching amplifier can be compactized as it utilizes the switching amplifying principle in which the transistor is operated constantly at a minimum heat-generating region. This arrangement obviates the need of providing any expensive position displacement sensor and power amplifier. Therefore, an inexpensive magnetic bearing can be readily implemented having a contactless, non-friction and oilless feature.
- The other objects and advantages will be apparent from the following description taken in conjunction with the accompanying drawings in which:
- Fig. 1 is a schematic diagram showing a non-linear control type magnetic bearing according to a first embodiment of this invention;
- Fig. 2 is a block diagram showing an operating circuit of the first embodiment of this invention;
- Figs. 3A and 3B are graphs showing a relation of a velocity dx/dt to an object displacement x and a relation of excitation current through an electromagnet coil to a time t when the non-linear control type magnetic bearing is operated with the use of a special switching discriminant;
- Figs. 4A and 4B are graphs showing a relation between the object displacement x and the velocity (dx/dt) and relation of excitation current through the electromagnet coil to a time t when the non-linear control type magnetic bearing is operated with the use of another special switching discriminant;
- Figs. 5A to 5D show graphs a relation of the object displacement x to the velocity dx/dt, a relation of the velocity dx/dt to the acceleration d2 x/dt2, a relation of the displacement x and estimated displacement y to the time t, and a relation of excitation current through the electromagnet coil to the time t, when the non-linear control type magnetic bearing, according to this invention, is operated under no disturbance with the use of the switching discriminant;
- Figs. 6A to 6E are graphs showing a relation of the object displacement x to the velocity dx/dt, a relation of the velocity dx/dt to the acceleration d 2x/dt2, a relation of the estimated displacement y to the time t, a relation of the displacement x to the time t, and a relation of excitation current through the electromagnet coil to the time t, when the non-linear control type magnetic bearing is operated under the gravitational field as a disturbance using the switching discriminant according to this invention;
- Fig. 7 is a schematic diagram showing a non-linear control type magnetic bearing according to a second embodiment of this invention; and
- Fig. 8 is a block diagram showing an operating circuit of the second embodiment of this invention.
- The non-linear control type magnetic bearing according to the first embodiment of this invention will be explained below by referring to Figs. 1 and 2.
- First and
12 and 14 are arranged opposite to each other in a manner to sandwich ansecond electromagnets object 10 therebetween with a gap left there. Coils of the first and 12 and 14 are connected at one end to one terminal of asecond electromagnets power supply 16. The coil of thefirst electromagnet 12 is connected at the other end to an Sl terminal of achangeover switch 20 through afirst resistor 18 for current detection and the coil of thesecond electromagnet 14 is connected at the other end to an S2 terminal of thechangeover switch 20 through asecond resistor 22 for current detection. An SO terminal of thechangeover switch 20 is connected to the other terminal of thepower supply 16. Thefirst electromagnet 12 is excited with the Sl terminal of thechangeover switch 20 in the ON state and thesecond electromagnet 14 is excited with the S2 terminal of thechangeover switch 20 in the ON state. That is, the first and 12 and 14 are excited alternately. In this connection it is to be noted that thesecond electromagnets changeover switch 20 is comprised of, for example, a transistor as a switching element. - Voltages across the first and
18 and 22 for current detection are supplied, as current level signals iA and iB, to ansecond resistors operating circuit 24. Avelocity sensor 26 comprised of, for example, a search coil is disposed opposite to the lower surface of theobject 10. The velocity with which theobject 10 is moved up and down is detected by thevelocity sensor 26 and a velocity signal dx/dt is supplied to theoperating circuit 24. - . The
operating circuit 24 is comprised of asubtracter 28,differentiator 30,analog operating circuit 32 and switchingdiscriminator 34, as shown in Fig. 2. The current level signals iA and iB detected are delivered to thesubtracter 28 where a calculation of i = iA-iB is carried out. A difference signal i as an output of thesubtracter 28 is supplied to theanalog operating circuit 32. A velocity signal dx/dt which is detected at thevelocity sensor 26 is supplied to thedifferentiator 30 where it is differentiated. The differentiated signal is supplied as the acceleration signal d2x/dt2, together with the current level signal, to theanalog operating circuit 32. In theanalog operating circuit 32, the current level signal i and acceleration signal d2x/dt2 are substituted into the equation of motion of theobject 10 to effect an analog operation and thus to produce a position displacement signal x of theobject 10. The position displacement signal x is supplied, together with the velocity signal dx/dt, to the switchingdiscriminator 34. Theswitching discriminator 34 identifies the positive or negative sign of a linear equation for the position displacement signal and velocity signal, and supplies to the changeover switch 20 a switching signal which alternately switches a supply of current to the electromagnets. It is to be noted that anorigin 0 in the position displacement of the object is determined to be located at an equilibrium point of theobject 10 as shown in Fig. 1. - The function and operation of the magnetic bearing of this invention will be explained below.
- First, an explanation will be given of the optimal control theory in general. A force acting on the
object 10 is comprised of a gravitational force and electromagnetic force. Now suppose only the electromagnetic force with the gravitational force disregarded here. Then, the equation of motion of theobject 10 is given below: where - m : the mass of the
object 10 to be levitated; and - M(x): the function of the displacement x including the coil impedance of the electromagnet.
- Differentiating the velocity signal dx/dt of the
velocity sensor 26 yields an acceleration d2 x/dt2. The current levels on the 12 and 14 can be normally measured. M(x) is found through the use of Equation (1). Since the function of M(x) is known beforehand, it is possible to evaluate the displacement x. In this way, the displacement x is evaluated from the current level I and velocity dx/dt. In order to determine the switching timing of therespective electromagnets changeover switch 20 through the use of the displacement x and velocity signal dx/dt, use is made of the optimal control theory. According to the optimal control theory, the switch changeover discriminant for minimum time control of movement of the object in a field of motion of an equation: is given by: - F(x, dx/dt) = m dx/dtl dx/dt + fx = 0 ... (3)
- Thus, the optimal control is realized if switching is effected to f at F(x, dx/dt) > 0 or -f at F(x, dx/dt) < 0. Here, f represents a constant.
- In this way it is possible to realize the optimal control in general. However, if the above-mentioned theory applies, the right-handed side of Equation (1) is not a constant, but a function for the current level and position, presenting a problem. For convenience, let us now consider a bearing system satisfying, in place of Equation (1), the following equation:
- This equation is obtained in the cases where permanent magnets are used also as electromagnets and where the attractive force of the electromagnet is linearized for the current level I. The essence of this invention is not affected even if Equation (4) is used in place of Equation (1). A subsequent explanation will be made based on this fact. The current level I flowing upon the application of a voltage e across the
12 and 14 is given by:electromagnets where - R : the resistance of the coil,
- L = L(x) : the inductance of the coil.
- Since, in general, the coil has an inductance, the current level reveals a time lag. The following explanation is based on the assumption that there is, as an ideal state, no time delay of the current. If Equation (4) is integrated once with L = 0 and I = ±10 (constant), then an equation:
is obtained as an optimal switching discriminant. - A control system of a smaller extent of delay and control system of a greater extent of delay were simulated using Equation (6). Figs. 3A and 3B and Figs. 4A and 4B show the loci of the simulations in the phase plane.
- When the coil has a small time constant (L/R) and then a time delay of the current is small, the
changeover switch 20 is switched to the Sl side at an initial level point A to permit the energization of theelectromagnet 12 as shown in Fig. 3A. At the level point C, thechangeover switch 20 is switched to the S2 side to permit the energization of theelectromagnet 14. Thereafter, the displacement x of the object immediately reaches atarget position 0 and thus an optimal control is realized with minimum time. This will be also well understood from the current level variation of the 12 and 14 as shown in Fig. 3B. After the displacement x of the object has arrived at the 0 point, this state (the 0 state) is maintained by the frequent switching operations. However, this system is not suitable for a smaller electric power, because the maximum current normally flows through either of theelectromagnets 12 and 14. In Fig. 3A, it is to be noted that the broken line P represents a switching curve and that the time tl corresponds to the point C.electromagnets - Figs. 4A and 4B show the operation of the
object 10 and the time variation of a current through the coil of the electromagnet (12, 14) when the time constant (T = L/R) of the coil of the electromagnets is greater (L » R > 0) and thus the time delay of the current is greater. In this case, use is made of the same switching curve P as shown in Fig. 3. This system is subject to an adverse influence resulting from the time delay of the current and thus a final limit cycle is involved, causing a greater vibration and positioning error. In other words, this system is not practical due to the involving of the limit cycle. - According to this invention, these problems are solved through the positive utilization of the phenomenon (Figs. 3A and 3B and Figs. 4A and 4B) which results from the time delay of the current level. That is, the embodiment of this invention adopts a
switching line 0 with a limited gradient with respect to anorigin 0 as shown in Fig. 5A. In Fig. 5A, the switching curve P is shown for guidance only and can be derived from Equation (6). This is of the same type as shown in Figs. 3A and 4A. The switching curve P has an infinite gradient at theorigin 0 and is different from the switching curve Q in this embodiment. Here, the switching curve Q becomes a linear function for the displacement x and velocity signal dx/dt and thus is represented as follows: - Using the displacement signal x from the
analog operating circuit 32 and velocity signal dx/dt from thevelocity sensor 26, the positive or negative sign of H(x, dx/dt) is judged at the switchingdiscriminator 34. With H(x, dx/dt) at the positive sign the terminal S2 of thechangeover switch 20 is rendered ON and with H(x, dx/dt) at the negative sign the terminal Sl is rendered ON. In consequence, as shown in Fig. 5A the displacement of theobject 10 converges from an initial level at a point A to a target level at thepoint 0, leaving no limit cycle behind. Fig. 5B shows a relation of the velocity signal dx/dt to the acceleration signal d2 x/dt2. From this figure it is found that theobject 10 converges toward anequilibrium point 0. Fig. 5C shows a relation of the displacement x of the object to the time t. From Fig. 5C it is also found that the displacement of theobject 10 converges toward theequilibrium point 0. Fig. 5D shows a variation of excitation currents iA, iB to the time t. From a comparison between Fig. 5D and Figs. 3B and 4B, it will be appreciated that the system of this embodiment needs a very small level of excitation current. Therefore, the embodiment of this invention, though being somewhat lower in response characteristics, can achieve a stability and a small power dissipation of practical importance. Furthermore, since the switching discriminant H(x, dx/dt) is the linear function of the displacement x and velocity signal dx/dt, it is possible to very readily effect an analog computation. The value y in Fig. 5C is an estimated value of the control system which is obtained by finding the position of the object through the use of the equation of motion (1) under the assumption that there is no disturbance. The actual displacement x of theobject 10 is in agreement with the estimated value y, provided that there is no disturbance. - An explanation has so far been made as to the embodiment of this invention under the assumption that there is no disturbance. Now an explanation will be given below with reference to Figs. 6A through 6E where the system of this invention is put under, for example, the gravitational field.
- In this case, the
object 10 is automatically moved to a position B where, as shown in Fig. 6A, the electromagnetic force of the 12 and 14 and gravity are in static equilibrium, with the result that theelectromagnets object 10 is maintained at the position B. Fig. 6B shows a relation of the velocity dx/dt to the acceleration d2x/dt2. As shown in Fig. 6C, the estimated value y of the control system varies with the time t and theobject 10 reaches an equilibrium point as shown in Fig. 6D. The excitation current of the coils varies as shown in Fig. 6E. It is to be noted that the ON time of theelectromagnet 12 is somewhat longer than that of theelectromagnet 14. - As evident from Fig. 6E, the dissipation current makes no appreciable difference even in the presence of the disturbance as compared with that in the absence of it. This is a marked advantage which can be obtained from the system of this invention.
- According to this invention, the
object 10 can be magnetically levitated by controlling thechangeover switch 20 using a switching discrimination signal generated in theoperating circuit 24. In this case, the currents through the 12 and 14 are reduced to a very small level due to the impedance of the coils, thus involving a very small dissipation power. Therefore, the non-linear control type magnetic bearing of low cost can be implemented without the need of providing any expensive position displacement sensor and power amplifier.electromagnets - A non-linear control type magnetic bearing according to a second embodiment of this invention will be explained below by referring to Figs. 7 and 8.
- In this embodiment, a judging
circuit 40 is connected between a terminal SO of achangeover switch 20 and the end of apower supply 16 and adapted to judge whether or not the current from thepower supply 16 continues for over a predetermined period of time at maximum. The judgment data is supplied to a switchingdiscriminator 34 in anoperating circuit 24. Theobject 10 can surely be levitated from an at-rest position under the action of the judgingcircuit 40 andoperating circuit 24. The other arrangement of this embodiment is the same as that of the first embodiment of this invention. Therefore, further explanation is omitted. - The operation of the second embodiment will be explained below. Now suppose that, at rest, the
object 10 is located, for example, on the side of theelectromagnet 14 and thechangeover switch 20 is placed on the side of the S2 terminal. Then, since the output of thevelocity sensor 26 is 0, no immediate switching occurs at thechangeover switch 20. During this time period, a maximum current continuously flows through theelectromagnet 14 and the judgingcircuit 40 judges this state. The judgment data is supplied to the switchingdiscriminator 34, causing thechangeover switch 20 to be forcedly switched to the Sl terminal of theswitch 20. Thereafter, theobject 10 is automatically moved to aposition 0 in the same way as explained in connection with Figs. 6A through 6E, and starts to be levitated. - This invention is not restricted to the above-mentioned embodiments. For example, a power relay may be used as the changeover switch in place of the transistor. The judging
circuit 40 is not required to be connected between thepower supply 16 and thechangeover switch 20, and may be placed anywhere in the associated circuit so long as it can judge that maximum current flows through either of the 12, 14 for over a predetermined period of time. Various changes or modifications can be made within the spirit and scope of this invention.electromagnets
Claims (7)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP14398184A JPS6124816A (en) | 1984-07-11 | 1984-07-11 | Nonlinear control type magnetic bearing |
| JP143981/84 | 1984-07-11 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| EP0168145A2 true EP0168145A2 (en) | 1986-01-15 |
| EP0168145A3 EP0168145A3 (en) | 1988-07-27 |
| EP0168145B1 EP0168145B1 (en) | 1991-04-17 |
Family
ID=15351537
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP85303636A Expired - Lifetime EP0168145B1 (en) | 1984-07-11 | 1985-05-23 | Non-linear control type magnetic bearing |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US4623202A (en) |
| EP (1) | EP0168145B1 (en) |
| JP (1) | JPS6124816A (en) |
| CA (1) | CA1231162A (en) |
| DE (1) | DE3582522D1 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2632354A1 (en) * | 1988-06-06 | 1989-12-08 | Mecanique Magnetique Sa | Device forming a follower seal for a rotating machine |
| EP0549912A1 (en) * | 1992-01-03 | 1993-07-07 | British Nuclear Fuels PLC | Apparatus for the electromagnetic control of the suspension of an object |
| FR2742497A1 (en) * | 1995-12-18 | 1997-06-20 | Aerospatiale | MAGNETIC BEARING WITH ALTERNATE ACTUATORS AND SENSORS |
| WO2011016850A1 (en) * | 2009-08-06 | 2011-02-10 | Geokinetics Acquisition Company | Magnetic mass-lift impulsive seismic energy source including attracting and repulsing electromagnets |
| CN113833757A (en) * | 2021-09-23 | 2021-12-24 | 北京航空航天大学 | Five-degree-of-freedom rotor axial displacement self-sensing magnetic suspension bearing |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL8601195A (en) * | 1986-05-12 | 1987-12-01 | Stichting Tech Wetenschapp | ELECTROMAGNETIC VIBRATOR FOR SEISMIC AND CIVIL TECHNICAL APPLICATIONS. |
| US5262692A (en) * | 1992-04-13 | 1993-11-16 | Center For Innovative Technology | Variable voltage switched current control |
| US5696412A (en) * | 1993-10-20 | 1997-12-09 | Iannello; Victor | Sensor-less position detector for an active magnetic bearing |
| US5495221A (en) * | 1994-03-09 | 1996-02-27 | The Regents Of The University Of California | Dynamically stable magnetic suspension/bearing system |
| US5736800A (en) * | 1994-10-18 | 1998-04-07 | Iannello; Victor | Light weight, high performance radial actuator for magnetic bearing systems |
| US5921505A (en) * | 1996-12-02 | 1999-07-13 | Trw Inc. | System and method for reducing mechanical disturbances from energy storage flywheels |
| US6472777B1 (en) * | 1998-08-25 | 2002-10-29 | Nikon Corporation | Capacitive sensor calibration method and apparatus for opposing electro-magnetic actuators |
| US6069417A (en) * | 1998-08-27 | 2000-05-30 | Nikon Corporation | Stage having paired E/I core actuator control |
| US6373676B1 (en) * | 1998-10-05 | 2002-04-16 | Span Inc. | Magnetic floatation control system |
| JP4521846B2 (en) * | 2000-08-18 | 2010-08-11 | 健蔵 野波 | Electromagnetic suction type magnetic bearing and its nonlinear control method |
| JP5003879B2 (en) * | 2007-03-30 | 2012-08-15 | 株式会社Ihi | Electromagnetic suction type magnetic bearing and its control method |
| CN114738385B (en) * | 2022-04-28 | 2023-03-21 | 珠海格力电器股份有限公司 | Magnetic suspension bearing system, control method and device thereof and storage medium |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3090239A (en) * | 1955-05-12 | 1963-05-21 | Bill Jack Scient Instr Co | Accelerometer |
| US3785709A (en) * | 1972-06-07 | 1974-01-15 | North American Rockwell | Force-position decoupler for electrostatic gyroscope suspension system |
| US3787100A (en) * | 1972-12-11 | 1974-01-22 | Armement Direction Tech Engins | Devices including rotating members supported by magnetic bearings |
| US3937533A (en) * | 1974-02-08 | 1976-02-10 | The United States Of America As Represented By The United States National Aeronautics And Space Administration Office Of General Counsel-Code Gp | Axially and radially controllable magnetic bearing |
| DE2537597A1 (en) * | 1975-08-23 | 1977-03-03 | Padana Ag | ELECTROMAGNETIC STORAGE DEVICE |
| US4078436A (en) * | 1976-02-27 | 1978-03-14 | Honeywell Inc. | Adaptive bias for electrically suspended gyroscope |
| JPS56150617A (en) * | 1980-04-22 | 1981-11-21 | Seiko Instr & Electronics Ltd | Control system for zero power magnetic bearing |
| US4379598A (en) * | 1980-12-22 | 1983-04-12 | North American Philips Corporation | Magnetic bearing |
| JPS57116931A (en) * | 1981-01-12 | 1982-07-21 | Nippon Seiko Kk | Controllable support system |
| DE3130974A1 (en) * | 1981-08-05 | 1983-02-24 | Teldix Gmbh, 6900 Heidelberg | MAGNETIC BEARING |
| JPS59117915A (en) * | 1982-12-22 | 1984-07-07 | Hitachi Ltd | magnetic bearing device |
-
1984
- 1984-07-11 JP JP14398184A patent/JPS6124816A/en active Granted
-
1985
- 1985-05-22 US US06/736,858 patent/US4623202A/en not_active Expired - Lifetime
- 1985-05-22 CA CA000482077A patent/CA1231162A/en not_active Expired
- 1985-05-23 DE DE8585303636T patent/DE3582522D1/en not_active Expired - Lifetime
- 1985-05-23 EP EP85303636A patent/EP0168145B1/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2632354A1 (en) * | 1988-06-06 | 1989-12-08 | Mecanique Magnetique Sa | Device forming a follower seal for a rotating machine |
| EP0549912A1 (en) * | 1992-01-03 | 1993-07-07 | British Nuclear Fuels PLC | Apparatus for the electromagnetic control of the suspension of an object |
| FR2742497A1 (en) * | 1995-12-18 | 1997-06-20 | Aerospatiale | MAGNETIC BEARING WITH ALTERNATE ACTUATORS AND SENSORS |
| EP0780587A1 (en) * | 1995-12-18 | 1997-06-25 | AEROSPATIALE Société Nationale Industrielle | Magnetic bearing with actuators and alterned sensors |
| US5763972A (en) * | 1995-12-18 | 1998-06-09 | Aerospatiale Societe Nationale Industrielle | Magnetic bearing with alternating actuators and sensors |
| WO2011016850A1 (en) * | 2009-08-06 | 2011-02-10 | Geokinetics Acquisition Company | Magnetic mass-lift impulsive seismic energy source including attracting and repulsing electromagnets |
| US8228762B2 (en) | 2009-08-06 | 2012-07-24 | Geokinetics Acquisition Company | Magnetic mass-lift impulsive seismic energy source including attracting and repulsing electromagnets |
| CN113833757A (en) * | 2021-09-23 | 2021-12-24 | 北京航空航天大学 | Five-degree-of-freedom rotor axial displacement self-sensing magnetic suspension bearing |
Also Published As
| Publication number | Publication date |
|---|---|
| DE3582522D1 (en) | 1991-05-23 |
| EP0168145B1 (en) | 1991-04-17 |
| JPH0510530B2 (en) | 1993-02-10 |
| CA1231162A (en) | 1988-01-05 |
| US4623202A (en) | 1986-11-18 |
| JPS6124816A (en) | 1986-02-03 |
| EP0168145A3 (en) | 1988-07-27 |
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